ardupilot/libraries/AP_Motors/AP_MotorsMulticopter.h

/// @file	AP_MotorsMulticopter.h
/// @brief	Motor control class for Multicopters
#pragma once

#include "AP_Motors_Class.h"
#include "AP_Motors_Thrust_Linearization.h"

#define AP_MOTORS_YAW_HEADROOM_DEFAULT  200
#define AP_MOTORS_THST_EXPO_DEFAULT     0.65f   // set to 0 for linear and 1 for second order approximation
#define AP_MOTORS_THST_HOVER_DEFAULT    0.35f   // the estimated hover throttle, 0 ~ 1
#define AP_MOTORS_THST_HOVER_TC         10.0f   // time constant used to update estimated hover throttle, 0 ~ 1
#define AP_MOTORS_THST_HOVER_MIN        0.125f  // minimum possible hover throttle
#define AP_MOTORS_THST_HOVER_MAX        0.6875f // maximum possible hover throttle
#define AP_MOTORS_SPIN_MIN_DEFAULT      0.15f   // throttle out ratio which produces the minimum thrust.  (i.e. 0 ~ 1 ) of the full throttle range
#define AP_MOTORS_SPIN_MAX_DEFAULT      0.95f   // throttle out ratio which produces the maximum thrust.  (i.e. 0 ~ 1 ) of the full throttle range
#define AP_MOTORS_SPIN_ARM_DEFAULT      0.10f   // throttle out ratio which produces the armed spin rate.  (i.e. 0 ~ 1 ) of the full throttle range
#define AP_MOTORS_BAT_VOLT_MAX_DEFAULT  0.0f    // voltage limiting max default
#define AP_MOTORS_BAT_VOLT_MIN_DEFAULT  0.0f    // voltage limiting min default (voltage dropping below this level will have no effect)
#define AP_MOTORS_BAT_CURR_MAX_DEFAULT  0.0f    // current limiting max default
#define AP_MOTORS_BAT_CURR_TC_DEFAULT   5.0f    // Time constant used to limit the maximum current
#define AP_MOTORS_SLEW_TIME_DEFAULT     0.0f    // slew rate limit for thrust output
#define AP_MOTORS_SAFE_TIME_DEFAULT     1.0f    // Time for the esc when transitioning between zero pwm to minimum

// spool definition
#define AP_MOTORS_SPOOL_UP_TIME_DEFAULT 0.5f    // time (in seconds) for throttle to increase from zero to min throttle, and min throttle to full throttle.

/// @class      AP_MotorsMulticopter
class AP_MotorsMulticopter : public AP_Motors {
public:

    // Constructor
    AP_MotorsMulticopter(uint16_t speed_hz = AP_MOTORS_SPEED_DEFAULT);

    // output - sends commands to the motors
    virtual void        output() override;

    // output_min - sends minimum values out to the motors
    void                output_min() override;

    // set_yaw_headroom - set yaw headroom (yaw is given at least this amount of pwm)
    void                set_yaw_headroom(int16_t pwm) { _yaw_headroom.set(pwm); }

    // update_throttle_range - update throttle endpoints
    void                update_throttle_range();

    // update estimated throttle required to hover
    void                update_throttle_hover(float dt);
    virtual float       get_throttle_hover() const override { return constrain_float(_throttle_hover, AP_MOTORS_THST_HOVER_MIN, AP_MOTORS_THST_HOVER_MAX); }

    // passes throttle directly to all motors for ESC calibration.
    //   throttle_input is in the range of 0 ~ 1 where 0 will send get_pwm_output_min() and 1 will send get_pwm_output_max()
    void                set_throttle_passthrough_for_esc_calibration(float throttle_input);

    // returns maximum thrust in the range 0 to 1
    float               get_throttle_thrust_max() const { return _throttle_thrust_max; }

    // return true if spool up is complete
    bool spool_up_complete() const { return _spool_state == SpoolState::THROTTLE_UNLIMITED; }

    // output a thrust to all motors that match a given motor
    // mask. This is used to control tiltrotor motors in forward
    // flight. Thrust is in the range 0 to 1
    virtual void        output_motor_mask(float thrust, uint16_t mask, float rudder_dt);

    // get_motor_mask - returns a bitmask of which outputs are being used for motors (1 means being used)
    //  this can be used to ensure other pwm outputs (i.e. for servos) do not conflict
    virtual uint32_t    get_motor_mask() override;

    // get minimum or maximum pwm value that can be output to motors
    int16_t             get_pwm_output_min() const { return _pwm_min; }
    int16_t             get_pwm_output_max() const { return _pwm_max; }
    
    // parameter check for MOT_PWM_MIN/MAX, returns true if parameters are valid
    bool check_mot_pwm_params() const;

    // set thrust compensation callback
    FUNCTOR_TYPEDEF(thrust_compensation_fn_t, void, float *, uint8_t);
    void                set_thrust_compensation_callback(thrust_compensation_fn_t callback) {
        _thrust_compensation_callback = callback;
    }
    
    // disable the use of motor torque to control yaw. Used when an external mechanism such
    // as vectoring is used for yaw control
    virtual void        disable_yaw_torque(void) {}

    // return whether a motor is enabled or not
    bool                is_motor_enabled(uint8_t i) override { return motor_enabled[i]; }

    // convert values to PWM min and max if not configured
    void                convert_pwm_min_max_param(int16_t radio_min, int16_t radio_max);

    // return thrust for motor motor_num, returns true if value is valid false otherwise
    bool                get_thrust(uint8_t motor_num, float& thr_out) const override;

#if HAL_LOGGING_ENABLED
    // 10hz logging of voltage scaling and max trust
    void                Log_Write() override;
#endif

    // Run arming checks
    bool arming_checks(size_t buflen, char *buffer) const override;

    // Getters for AP_Motors example, not used by vehicles
    float get_throttle_avg_max() const;
    int16_t get_yaw_headroom() const;

    // Thrust Linearization handling
    Thrust_Linearization thr_lin {*this};

    // var_info for holding Parameter information
    static const struct AP_Param::GroupInfo        var_info[];

protected:

    // run spool logic
    void                output_logic();

    // output_to_motors - sends commands to the motors
    virtual void        output_to_motors() = 0;

    // update the throttle input filter
    virtual void        update_throttle_filter() override;

    // return current_limit as a number from 0 ~ 1 in the range throttle_min to throttle_max
    virtual float       get_current_limit_max_throttle();

    // convert actuator output (0~1) range to pwm range
    int16_t             output_to_pwm(float _actuator_output);

    // adds slew rate limiting to actuator output if MOT_SLEW_TIME > 0 and not shutdown
    void                set_actuator_with_slew(float& actuator_output, float input);

    // gradually increase actuator output to ground idle
    float               actuator_spin_up_to_ground_idle() const;

    // apply any thrust compensation for the frame
    virtual void        thrust_compensation(void) {}

    // output booster throttle, if any
    virtual void        output_boost_throttle(void);

    // output roll/pitch/yaw/thrust
    virtual void        output_rpyt(void);

    // save parameters as part of disarming
    void                save_params_on_disarm() override;

    // update external limits from scripting
    void                update_external_limits();

    // enum values for HOVER_LEARN parameter
    enum HoverLearn {
        HOVER_LEARN_DISABLED = 0,
        HOVER_LEARN_ONLY = 1,
        HOVER_LEARN_AND_SAVE = 2
    };

    // parameters
    AP_Int16            _yaw_headroom;          // yaw control is given at least this pwm range
    AP_Float            _slew_up_time;          // throttle increase slew limitting
    AP_Float            _slew_dn_time;          // throttle decrease slew limitting
    AP_Float            _safe_time;             // Time for the esc when transitioning between zero pwm to minimum
    AP_Float            _spin_arm;              // throttle out ratio which produces the armed spin rate.  (i.e. 0 ~ 1 ) of the full throttle range
    AP_Float            _batt_current_max;      // current over which maximum throttle is limited
    AP_Float            _batt_current_time_constant;    // Time constant used to limit the maximum current
    AP_Int16            _pwm_min;               // minimum PWM value that will ever be output to the motors (if 0, vehicle's throttle input channel's min pwm used)
    AP_Int16            _pwm_max;               // maximum PWM value that will ever be output to the motors (if 0, vehicle's throttle input channel's max pwm used)
    AP_Float            _throttle_hover;        // estimated throttle required to hover throttle in the range 0 ~ 1
    AP_Int8             _throttle_hover_learn;  // enable/disabled hover thrust learning
    AP_Int8             _disarm_disable_pwm;    // disable PWM output while disarmed

    // Maximum lean angle of yaw servo in degrees. This is specific to tricopter
    AP_Float            _yaw_servo_angle_max_deg;

    // time to spool motors to min throttle
    AP_Float            _spool_up_time;
    AP_Float            _spool_down_time;

    // scaling for booster motor throttle
    AP_Float            _boost_scale;

    // motor output variables
    bool                motor_enabled[AP_MOTORS_MAX_NUM_MOTORS];    // true if motor is enabled

    // spool variables
    float               _spin_up_ratio;      // throttle percentage (0 ~ 1) between zero and throttle_min

    // battery voltage, current and air pressure compensation variables
    float               _throttle_limit;        // ratio of throttle limit between hover and maximum
    float               _throttle_thrust_max;   // the maximum allowed throttle thrust 0.0 to 1.0 in the range throttle_min to throttle_max
    float               _disarm_safe_timer;     // Timer for the esc when transitioning between zero pwm to minimum

    // vehicle supplied callback for thrust compensation. Used for tiltrotors and tiltwings
    thrust_compensation_fn_t _thrust_compensation_callback;

    // array of motor output values
    float _actuator[AP_MOTORS_MAX_NUM_MOTORS];

    /* motor enabled, checking the override mask
       _motor_mask_override is only set for tilt quadplanes
     */
    bool motor_enabled_mask(uint8_t i) const {
        return motor_enabled[i] && (_motor_mask_override & (1U << i)) == 0;
    }

    // mask of overridden motors (used by quadplane tiltrotors)
    uint16_t _motor_mask_override;
};